============ KPT ================= TIME: Thu Jun 11 16:45:36 2009 USER: Todd Ansty ================================== Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090507AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00131.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/input.ivt Successfully Read TLF File: /export/home/eros/PDT13.3d/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_param.ssid Successfully Read Input PEF File: pdt_Run_5/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090507AP_RE_90165_18018.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/090202BP_IRRE_00256_50017.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_PE_08138_10182.bsp Insert Spice File: /cas/ancillary/ops/NAIF/sp/080806AP_SK_08138_10182.bsp Insert Leap Seconds File: /cas/ancillary/ops/NAIF/lsk/naif0009.tls Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck15May2008.tpc Insert Physical Constants File: /cas/ancillary/ops/NAIF/pck/cpck_rock_11May2009_merged.tpc Insert SCLK SCET File: /cas/ancillary/ops/NAIF/sclk/cas00131.tsc SPICE Successfully Opened Successfully Read BVH File: pdt_Run_5/input.bvh Successfully Read IVT File: pdt_Run_5/input.ivt Successfully Read TLF File: /export/home/eros/PDT13.3d/Input/KPT/kpt_default.tlf Successfully Read KPT Spice Identification File: /cas/ancillary/ops/SCO/ssid/09_131_param.ssid Successfully Read Input PEF File: pdt_Run_5/temp.pef NOTE: This File Supercedes Any Events held within the Input Configuration File. Successfully Read KPT CMT File: /cas/ancillary/ops/SCO/cmt_limits/POST_PROBE_V11.cmt ------------------------------ CSAS-KPT Version: V13.1 ------------------------------ SID Suspend Values Theta_1: 0.20 degrees Theta_2: 0.50 degrees Theta_3: 1.50 degrees T_1: 60.00 seconds T_2: 240.00 seconds T_3: 1800.00 seconds T_4: 2400.00 seconds **** WARNING: INITIAL PRIMARY INERTIAL Vector TITAN is present in the Initial IVT, but the Vector Entry has a time interval which does NOT contain the Current Time of interest. THIS CONDITION REQUIRES FIXING IF THIS IS A REAL SEQUENCE. ************************************************************ NOTE: MANEUVER COMMANDS Cause Turning of the Spacecraft 1.125 -> 2.000 seconds following the Command Time - the times shown in this Run Log are times that the Spacecraft Actually Starts Turning. ************************************************************ ************************************************************ NOTE: CONSTRAINT MONITOR IS SELECTED FOR THIS RUN Initial CMT Dynamic Constraints: RCS Max Rates(rad/s): 1.43000000e-02 1.43000000e-02 1.43000000e-02 RCS Max Accel(rad/s/s): 1.52700000e-04 1.24200000e-04 3.24700000e-04 RWA Max Rates(rad/s): 2.46800000e-03 2.96200000e-03 4.88600000e-03 RWA Max Accel(rad/s/s): 1.35300000e-05 1.62300000e-05 2.67800000e-05 ************************************************************ ************************************************************ * * * NOTE: ALL ERRORS, REJECTED COMMANDS, WARNINGS, * * CMT VIOLATIONS, etc, MUST BE FIXED PRIOR * * TO FINAL SEQUENCE GENERATION and UPLINK * ************************************************************ Adding/Replacing Vector TITAN to the IVT at UTC Time: 2009-345T15:33:19.000 Adding/Replacing Vector TITAN_LAT_VIEW_130 to the IVT at UTC Time: 2009-345T15:57:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_130 to the IVT at UTC Time: 2009-345T15:57:59.000 PROCESSING Starting on PROFILE Command at 2084.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:03:08.000 ) This is Command #1 from the Event List TARGET / Command #2: Primary Inertial Vector: TITAN_LAT_VIEW_130 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #2: Secondary Inertial Vector: TITAN_FOV_LIMB_130 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2085.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:03:09.000 ) This is Command #2 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_130; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_130; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2092.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:03:16.000 ) This is Command #3 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 97.5192 PROCESSING Starting on 89EXE_CMD_SEQ Command at 2090.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:03:14.000 ) This is Command #4 from the Event List Simulated Maneuver End Time (UTC): 2009-345T16:04:53.750 Turn Magnitude for 7OFFSET (milliradians): 25.1438 Adding/Replacing Vector TITAN_LAT_VIEW_131 to the IVT at UTC Time: 2009-345T16:08:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_131 to the IVT at UTC Time: 2009-345T16:08:59.000 PROCESSING Starting on OFFSET Command at 2467.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:09:31.000 ) This is Command #5 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2796 Simulated Maneuver End Time (UTC): 2009-345T16:10:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4790 PROCESSING Starting on PROFILE Command at 2744.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:14:08.000 ) This is Command #6 from the Event List TARGET / Command #7: Primary Inertial Vector: TITAN_LAT_VIEW_131 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #7: Secondary Inertial Vector: TITAN_FOV_LIMB_131 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 2745.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:14:09.000 ) This is Command #7 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_131; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_131; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 2752.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:14:16.000 ) This is Command #8 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.7103 Simulated Maneuver End Time (UTC): 2009-345T16:17:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.4106 Adding/Replacing Vector TITAN_LAT_VIEW_132 to the IVT at UTC Time: 2009-345T16:20:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_132 to the IVT at UTC Time: 2009-345T16:20:59.000 PROCESSING Starting on OFFSET Command at 3187.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:21:31.000 ) This is Command #9 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2795 Simulated Maneuver End Time (UTC): 2009-345T16:22:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4745 PROCESSING Starting on PROFILE Command at 3464.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:26:08.000 ) This is Command #10 from the Event List TARGET / Command #11: Primary Inertial Vector: TITAN_LAT_VIEW_132 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #11: Secondary Inertial Vector: TITAN_FOV_LIMB_132 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 3465.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:26:09.000 ) This is Command #11 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_132; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_132; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 3472.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:26:16.000 ) This is Command #12 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6473 Simulated Maneuver End Time (UTC): 2009-345T16:29:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3465 Adding/Replacing Vector TITAN_LAT_VIEW_133 to the IVT at UTC Time: 2009-345T16:32:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_133 to the IVT at UTC Time: 2009-345T16:32:59.000 PROCESSING Starting on OFFSET Command at 3907.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:33:31.000 ) This is Command #13 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2794 Simulated Maneuver End Time (UTC): 2009-345T16:34:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4699 PROCESSING Starting on PROFILE Command at 4184.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:38:08.000 ) This is Command #14 from the Event List TARGET / Command #15: Primary Inertial Vector: TITAN_LAT_VIEW_133 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #15: Secondary Inertial Vector: TITAN_FOV_LIMB_133 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4185.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:38:09.000 ) This is Command #15 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_133; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_133; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4192.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:38:16.000 ) This is Command #16 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6327 Simulated Maneuver End Time (UTC): 2009-345T16:41:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3324 Adding/Replacing Vector TITAN_LAT_VIEW_134 to the IVT at UTC Time: 2009-345T16:44:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_134 to the IVT at UTC Time: 2009-345T16:44:59.000 PROCESSING Starting on OFFSET Command at 4627.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:45:31.000 ) This is Command #17 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2793 Simulated Maneuver End Time (UTC): 2009-345T16:46:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4653 PROCESSING Starting on PROFILE Command at 4904.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:50:08.000 ) This is Command #18 from the Event List TARGET / Command #19: Primary Inertial Vector: TITAN_LAT_VIEW_134 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #19: Secondary Inertial Vector: TITAN_FOV_LIMB_134 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 4905.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:50:09.000 ) This is Command #19 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_134; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_134; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 4912.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:50:16.000 ) This is Command #20 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6277 Simulated Maneuver End Time (UTC): 2009-345T16:53:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3281 Adding/Replacing Vector TITAN_LAT_VIEW_135 to the IVT at UTC Time: 2009-345T16:56:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_135 to the IVT at UTC Time: 2009-345T16:56:59.000 PROCESSING Starting on OFFSET Command at 5347.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T16:57:31.000 ) This is Command #21 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2792 Simulated Maneuver End Time (UTC): 2009-345T16:58:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4608 PROCESSING Starting on PROFILE Command at 5624.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:02:08.000 ) This is Command #22 from the Event List TARGET / Command #23: Primary Inertial Vector: TITAN_LAT_VIEW_135 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #23: Secondary Inertial Vector: TITAN_FOV_LIMB_135 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 5625.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:02:09.000 ) This is Command #23 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_135; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_135; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 5632.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:02:16.000 ) This is Command #24 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6259 Simulated Maneuver End Time (UTC): 2009-345T17:05:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3272 Adding/Replacing Vector TITAN_LAT_VIEW_136 to the IVT at UTC Time: 2009-345T17:08:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_136 to the IVT at UTC Time: 2009-345T17:08:59.000 PROCESSING Starting on OFFSET Command at 6067.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:09:31.000 ) This is Command #25 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2791 Simulated Maneuver End Time (UTC): 2009-345T17:10:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4563 PROCESSING Starting on PROFILE Command at 6344.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:14:08.000 ) This is Command #26 from the Event List TARGET / Command #27: Primary Inertial Vector: TITAN_LAT_VIEW_136 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #27: Secondary Inertial Vector: TITAN_FOV_LIMB_136 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 6345.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:14:09.000 ) This is Command #27 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_136; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_136; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 6352.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:14:16.000 ) This is Command #28 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6256 Simulated Maneuver End Time (UTC): 2009-345T17:17:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3279 Adding/Replacing Vector TITAN_LAT_VIEW_137 to the IVT at UTC Time: 2009-345T17:20:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_137 to the IVT at UTC Time: 2009-345T17:20:59.000 PROCESSING Starting on OFFSET Command at 6787.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:21:31.000 ) This is Command #29 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2790 Simulated Maneuver End Time (UTC): 2009-345T17:22:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4519 PROCESSING Starting on PROFILE Command at 7064.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:26:08.000 ) This is Command #30 from the Event List TARGET / Command #31: Primary Inertial Vector: TITAN_LAT_VIEW_137 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #31: Secondary Inertial Vector: TITAN_FOV_LIMB_137 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 7065.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:26:09.000 ) This is Command #31 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_137; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_137; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 7072.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:26:16.000 ) This is Command #32 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6261 Simulated Maneuver End Time (UTC): 2009-345T17:29:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3296 Adding/Replacing Vector TITAN_LAT_VIEW_138 to the IVT at UTC Time: 2009-345T17:32:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_138 to the IVT at UTC Time: 2009-345T17:32:59.000 PROCESSING Starting on OFFSET Command at 7507.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:33:31.000 ) This is Command #33 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2789 Simulated Maneuver End Time (UTC): 2009-345T17:34:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4478 PROCESSING Starting on PROFILE Command at 7784.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:38:08.000 ) This is Command #34 from the Event List TARGET / Command #35: Primary Inertial Vector: TITAN_LAT_VIEW_138 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #35: Secondary Inertial Vector: TITAN_FOV_LIMB_138 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 7785.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:38:09.000 ) This is Command #35 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_138; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_138; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 7792.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:38:16.000 ) This is Command #36 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6273 Simulated Maneuver End Time (UTC): 2009-345T17:41:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3319 Adding/Replacing Vector TITAN_LAT_VIEW_139 to the IVT at UTC Time: 2009-345T17:44:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_139 to the IVT at UTC Time: 2009-345T17:44:59.000 PROCESSING Starting on OFFSET Command at 8227.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:45:31.000 ) This is Command #37 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2788 Simulated Maneuver End Time (UTC): 2009-345T17:46:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4438 PROCESSING Starting on PROFILE Command at 8504.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:50:08.000 ) This is Command #38 from the Event List TARGET / Command #39: Primary Inertial Vector: TITAN_LAT_VIEW_139 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #39: Secondary Inertial Vector: TITAN_FOV_LIMB_139 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 8505.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:50:09.000 ) This is Command #39 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_139; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_139; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 8512.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:50:16.000 ) This is Command #40 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6289 Simulated Maneuver End Time (UTC): 2009-345T17:53:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3348 Adding/Replacing Vector TITAN_LAT_VIEW_140 to the IVT at UTC Time: 2009-345T17:56:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_140 to the IVT at UTC Time: 2009-345T17:56:59.000 PROCESSING Starting on OFFSET Command at 8947.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T17:57:31.000 ) This is Command #41 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2787 Simulated Maneuver End Time (UTC): 2009-345T17:58:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4401 PROCESSING Starting on PROFILE Command at 9224.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:02:08.000 ) This is Command #42 from the Event List TARGET / Command #43: Primary Inertial Vector: TITAN_LAT_VIEW_140 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #43: Secondary Inertial Vector: TITAN_FOV_LIMB_140 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 9225.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:02:09.000 ) This is Command #43 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_140; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_140; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 9232.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:02:16.000 ) This is Command #44 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6312 Simulated Maneuver End Time (UTC): 2009-345T18:05:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3384 Adding/Replacing Vector TITAN_LAT_VIEW_141 to the IVT at UTC Time: 2009-345T18:08:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_141 to the IVT at UTC Time: 2009-345T18:08:59.000 PROCESSING Starting on OFFSET Command at 9667.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:09:31.000 ) This is Command #45 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2786 Simulated Maneuver End Time (UTC): 2009-345T18:10:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4367 PROCESSING Starting on PROFILE Command at 9944.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:14:08.000 ) This is Command #46 from the Event List TARGET / Command #47: Primary Inertial Vector: TITAN_LAT_VIEW_141 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #47: Secondary Inertial Vector: TITAN_FOV_LIMB_141 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 9945.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:14:09.000 ) This is Command #47 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_141; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_141; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 9952.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:14:16.000 ) This is Command #48 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6339 Simulated Maneuver End Time (UTC): 2009-345T18:17:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3426 Adding/Replacing Vector TITAN_LAT_VIEW_142 to the IVT at UTC Time: 2009-345T18:20:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_142 to the IVT at UTC Time: 2009-345T18:20:59.000 PROCESSING Starting on OFFSET Command at 10387.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:21:31.000 ) This is Command #49 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2785 Simulated Maneuver End Time (UTC): 2009-345T18:22:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4337 PROCESSING Starting on PROFILE Command at 10664.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:26:08.000 ) This is Command #50 from the Event List TARGET / Command #51: Primary Inertial Vector: TITAN_LAT_VIEW_142 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #51: Secondary Inertial Vector: TITAN_FOV_LIMB_142 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 10665.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:26:09.000 ) This is Command #51 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_142; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_142; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 10672.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:26:16.000 ) This is Command #52 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6373 Simulated Maneuver End Time (UTC): 2009-345T18:29:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3476 Adding/Replacing Vector TITAN_LAT_VIEW_143 to the IVT at UTC Time: 2009-345T18:32:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_143 to the IVT at UTC Time: 2009-345T18:32:59.000 PROCESSING Starting on OFFSET Command at 11107.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:33:31.000 ) This is Command #53 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2784 Simulated Maneuver End Time (UTC): 2009-345T18:34:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4312 PROCESSING Starting on PROFILE Command at 11384.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:38:08.000 ) This is Command #54 from the Event List TARGET / Command #55: Primary Inertial Vector: TITAN_LAT_VIEW_143 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #55: Secondary Inertial Vector: TITAN_FOV_LIMB_143 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 11385.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:38:09.000 ) This is Command #55 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_143; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_143; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 11392.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:38:16.000 ) This is Command #56 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6416 Simulated Maneuver End Time (UTC): 2009-345T18:41:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3535 Adding/Replacing Vector TITAN_LAT_VIEW_144 to the IVT at UTC Time: 2009-345T18:44:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_144 to the IVT at UTC Time: 2009-345T18:44:59.000 PROCESSING Starting on OFFSET Command at 11827.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:45:31.000 ) This is Command #57 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2784 Simulated Maneuver End Time (UTC): 2009-345T18:46:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4293 PROCESSING Starting on PROFILE Command at 12104.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:50:08.000 ) This is Command #58 from the Event List TARGET / Command #59: Primary Inertial Vector: TITAN_LAT_VIEW_144 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #59: Secondary Inertial Vector: TITAN_FOV_LIMB_144 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 12105.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:50:09.000 ) This is Command #59 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_144; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_144; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 12112.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:50:16.000 ) This is Command #60 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6468 Simulated Maneuver End Time (UTC): 2009-345T18:53:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3606 Adding/Replacing Vector TITAN_LAT_VIEW_145 to the IVT at UTC Time: 2009-345T18:56:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_145 to the IVT at UTC Time: 2009-345T18:56:59.000 PROCESSING Starting on OFFSET Command at 12547.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T18:57:31.000 ) This is Command #61 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2784 Simulated Maneuver End Time (UTC): 2009-345T18:58:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4280 PROCESSING Starting on PROFILE Command at 12824.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:02:08.000 ) This is Command #62 from the Event List TARGET / Command #63: Primary Inertial Vector: TITAN_LAT_VIEW_145 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #63: Secondary Inertial Vector: TITAN_FOV_LIMB_145 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 12825.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:02:09.000 ) This is Command #63 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_145; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_145; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 12832.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:02:16.000 ) This is Command #64 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6532 Simulated Maneuver End Time (UTC): 2009-345T19:05:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3692 Adding/Replacing Vector TITAN_LAT_VIEW_146 to the IVT at UTC Time: 2009-345T19:08:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_146 to the IVT at UTC Time: 2009-345T19:08:59.000 PROCESSING Starting on OFFSET Command at 13267.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:09:31.000 ) This is Command #65 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2783 Simulated Maneuver End Time (UTC): 2009-345T19:10:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4276 PROCESSING Starting on PROFILE Command at 13544.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:14:08.000 ) This is Command #66 from the Event List TARGET / Command #67: Primary Inertial Vector: TITAN_LAT_VIEW_146 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #67: Secondary Inertial Vector: TITAN_FOV_LIMB_146 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 13545.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:14:09.000 ) This is Command #67 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_146; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_146; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 13552.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:14:16.000 ) This is Command #68 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6612 Simulated Maneuver End Time (UTC): 2009-345T19:17:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3795 Adding/Replacing Vector TITAN_LAT_VIEW_147 to the IVT at UTC Time: 2009-345T19:20:54.000 Adding/Replacing Vector TITAN_FOV_LIMB_147 to the IVT at UTC Time: 2009-345T19:20:59.000 PROCESSING Starting on OFFSET Command at 13987.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:21:31.000 ) This is Command #69 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2784 Simulated Maneuver End Time (UTC): 2009-345T19:22:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4281 PROCESSING Starting on PROFILE Command at 14264.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:26:08.000 ) This is Command #70 from the Event List TARGET / Command #71: Primary Inertial Vector: TITAN_LAT_VIEW_147 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT TARGET / Command #71: Secondary Inertial Vector: TITAN_FOV_LIMB_147 determined by an Evaluation of Chebyshev Polynomials, which originate from the IVT PROCESSING Starting on TARGET Command at 14265.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:26:09.000 ) This is Command #71 from the Event List PRIMARY BODY: CIRS_FPB; PRIMARY INERTIAL: TITAN_LAT_VIEW_147; SECONDARY BODY: POS_Z; SECONDARY INERTIAL: TITAN_FOV_LIMB_147; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 14272.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:26:16.000 ) This is Command #72 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 170.6711 Simulated Maneuver End Time (UTC): 2009-345T19:29:06.870 Turn Magnitude for 7OFFSET (milliradians): 87.3923 PROCESSING Starting on OFFSET Command at 14707.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:33:31.000 ) This is Command #73 from the Event List QUANTIZED ANGLES: -2.492 0.000 0.000 mrad Profiled Maneuver time (seconds): 33.2784 Simulated Maneuver End Time (UTC): 2009-345T19:34:04.500 Turn Magnitude for 7OFFSET (milliradians): 2.4297 Adding/Replacing Vector TITAN to the IVT at UTC Time: 2009-345T19:39:29.000 PROCESSING Starting on PROFILE Command at 15354.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:44:18.000 ) This is Command #74 from the Event List PROCESSING Starting on TARGET Command at 15355.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:44:19.000 ) This is Command #75 from the Event List PRIMARY BODY: NEG_Y; PRIMARY INERTIAL: TITAN; SECONDARY BODY: NEG_X; SECONDARY INERTIAL: SUN; Light Time Correction: NO_COR PROCESSING Starting on OFFSET Command at 15362.000 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T19:44:26.000 ) This is Command #76 from the Event List QUANTIZED ANGLES: 0.000 0.000 0.000 mrad Profiled Maneuver time (seconds): 1092.9577 Adding/Replacing Vector CASSINI to the IVT at UTC Time: 2009-345T19:58:24.000 PROCESSING Starting on 89EXE_CMD_SEQ Command at 16430.004 Seconds Into the Simulated Maneuver Sequence. ( Spacecraft Event Time (UTC): 2009-345T20:02:14.000 ) This is Command #77 from the Event List Simulated Maneuver End Time (UTC): 2009-345T20:02:39.120 Turn Magnitude for 7OFFSET (milliradians): 1482.3245 EVENT SEQUENCE COMPLETED SUCCESSFULLY. (Save Checklist and Violations Summary Reports for more details) Created KPT Plot File: pdt_Run_5/kpt_eo.plt -----------------------------------